[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

EP3211452B1 - Device for detecting objects carried by an individual - Google Patents

Device for detecting objects carried by an individual Download PDF

Info

Publication number
EP3211452B1
EP3211452B1 EP17157293.6A EP17157293A EP3211452B1 EP 3211452 B1 EP3211452 B1 EP 3211452B1 EP 17157293 A EP17157293 A EP 17157293A EP 3211452 B1 EP3211452 B1 EP 3211452B1
Authority
EP
European Patent Office
Prior art keywords
radar
cylinder
guides
antenna
movable
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP17157293.6A
Other languages
German (de)
French (fr)
Other versions
EP3211452A1 (en
Inventor
Claude Chekroun
Gilles Chekroun
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SWS
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of EP3211452A1 publication Critical patent/EP3211452A1/en
Application granted granted Critical
Publication of EP3211452B1 publication Critical patent/EP3211452B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • G01S13/887Radar or analogous systems specially adapted for specific applications for detection of concealed objects, e.g. contraband or weapons
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/003Bistatic radar systems; Multistatic radar systems
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/86Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
    • G01S13/867Combination of radar systems with cameras
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • G01S13/89Radar or analogous systems specially adapted for specific applications for mapping or imaging
    • G01S13/90Radar or analogous systems specially adapted for specific applications for mapping or imaging using synthetic aperture techniques, e.g. synthetic aperture radar [SAR] techniques
    • G01S13/904SAR modes
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/03Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/42Housings not intimately mechanically associated with radiating elements, e.g. radome

Definitions

  • the two guides are engraved in a cylinder disposed inside the mobile cylinder, the two cylinders having the same axis, and the space between the two cylinders is equal to 0.1 mm ⁇ 0.05 mm.
  • Said rotary antenna comprises, for example, a system for minimizing microwave leakage, said system being composed of three cavities, said cavities being arranged in pairs on each side of said waveguides, parallel to these, along their entire length.
  • Said waveguides being engraved in a cylinder disposed inside the mobile cylinder, said mobile cylinder and said inner cylinder are for example rotatable by means of a ball bearing device, the base of said movable cylinder. and the base of said inner cylinder being respectively mechanically secured to the movable part and the fixed part of said device.
  • Said radar operates for example in a millimetric frequency band.
  • said device comprises two rotary antennas for said radar to operate in bi-static mode, one antenna transmitting and the other antenna being dedicated to reception.
  • the antennas are for example interconnected by two waveguides, a guide connecting the transmission guides of said antennas and the other guide connecting the reception guides, the first waveguide being connected via a magic T to a waveguide connected to the radar and the second waveguide being connected via another magic T to a waveguide connected to the radar.
  • Said radar emits, for example, according to a number N of frequencies close to a given frequency, the emission pulse being divided into N parts, each part corresponding to a frequency, a first level of analysis of the image being carried out for the signals received at the first of said frequencies, other analyzes being carried out for the signals received at the other frequencies, the various analyzes making it possible to approach the theoretical value of the dielectric permittivity of a detected object.
  • the computer is for example an integral part of the processing means of said radar.
  • Said device comprising means for displaying the images obtained, said viewing means are for example glasses worn by a user and on which said images are projected.
  • the antenna part, the radar and their interconnection means are arranged inside a portable cylindrical structure, also acting as a radome, said structure supporting said camera.
  • the Figures 2a and 2b illustrate the principle of possible realization of the scanner 1.
  • the figure 2 illustrates the principle of realization.
  • the antenna 1 comprises a metal cylinder 21 having a radiating opening 22 in a helical line 23 running around the cylinder.
  • the antenna comprises at least one pair of waveguides 24, 25 disposed inside the cylinder and open towards the inner wall of the cylinder.
  • a waveguide 24 is reserved for transmission and the other waveguide 25 is reserved for reception.
  • the transmission guide 24 is connected to the transmitting means of the radar 2 and the reception guide 25 is connected to the reception means of the radar 2.
  • the cylinder 21 and the waveguides 24, 25 have a relative rotational movement relative to the axis 100 of the cylinder.
  • the guides remain fixed and the cylinder 21 is rotated around the guides.
  • the guides 24, 25 are placed on a support 26 disposed inside the cylinder 21.
  • the figure 2b illustrates an exemplary embodiment of the support 26 of the waveguides 24, 25.
  • This support 26, disposed inside the first cylinder 21, is a cylinder. It forms the stator in the case where the first cylinder 21, the rotor, is driven by a rotational movement.
  • the waveguides 24, 25 are arranged on the inner cylinder 26. In a preferred embodiment, the guides 24, 25 are etched in this cylinder 26. In fact, given the speed of movement of the people to be monitored , from 0.5 to 3 km / h, to obtain a good sampling of the synthetic antenna, at 0.5 ⁇ ( ⁇ being the length of the microwave wave used), the speed of rotation of the rotor must be understood between 1500 and 3000 revolutions per minute, which excludes any asymmetry of the stator.
  • the antenna 1 comprises two guides 24, 25, one in transmission and the other in reception, these two distinct guides advantageously allowing a car real-time calibration. Indeed, any mechanical system operating at rotation speeds such as that previously announced requires a calibration system almost in real time.
  • This calibration requires the measurement of the different microwave paths inside the device which can be advantageously achieved by the external coupling between the emission produced by the transmission guide 24 and the reception on the other guide 25, thus enabling actions preventative measures against disturbances.
  • the figure 3 presents by a transverse view the arrangement of the inner cylinder 26 with respect to the outer cylinder 21, the two cylinders having the same axis of symmetry 100.
  • the diameter of the inner cylinder 26 is for example defined so that the radiating face of the guides is at a given distance from the outer cylinder that will be specified later.
  • this metallized face acts as a short microwave circuit, without preventing leaks at the contacts.
  • three slots are provided, engraved in the inner cylinder acting as short circuits making it possible to reduce short circuits to the level of the guides.
  • FIG. 6a and 6b An example of realization of these slots will be presented to Figures 6a and 6b .
  • the principle of realization of the rotary antenna illustrated by the Figures 2a, 2b and 3 uses a pair of waveguides 24, 25, one for transmission and the other for reception. It is possible to provide an embodiment comprising two pairs of waveguides (transmission and reception). In this case, the second pair is for example diametrically opposed to the first pair 24, 25.
  • the two pairs of guides are then for example connected to the radar 2 via an SP4T switch.
  • such an antenna makes it possible to increase the control domain.
  • the inner cylinder 26 comprising the two waveguides 24, 25 is fixed, the two guides being rectilinear.
  • the rotor 21 has the helical slot 22 which rotates around the guides. It is possible to provide an embodiment where the inner cylinder 26 equipped with rotating waveguides, forming a rotor, while the helical slot 22 remains fixed.
  • the waveguides have a helical shape and the slot in rotation around the guides is rectilinear. This rotational movement is relative, that is to say either the slots can be fixed and the slot rotatable, or conversely the guides are rotatable and the slot is fixed.
  • the hollow cylinder carrying the slot is fixed, it can act as a radome, also avoiding that the slot deforms under the effect of rotation.
  • Rotating waveguides require a rotating joint system and a mechanism adapted to exchange the signals with the radar.
  • the operating principle remains that described in Figures 4a to 4e . Subsequently, an embodiment according to the Figures 2a and 2b where the guides remain fixed.
  • the figures 5a and 5b presents an exemplary embodiment according to this embodiment, the figure 5a representing the fixed inner cylinder 26, stator, equipped with two waveguides 24, 25 and the figure 5b representing the outer cylinder 21, equipped with the helical slot, rotating around the fixed cylinder.
  • the outer cylinder 21 is rotated by a motor 19, shown in FIG. figure 1 . It slides in rotation relative to the fixed portion via a cylindrical ball bearing device 30.
  • the fixed portion 27 of the ball bearing is mechanically secured to the base of the inner cylinder 26 and the movable portion 27 'of the ball bearing is secured to mechanically of a support 28, for example of cylindrical shape, this support being itself mechanically secured to the outer cylinder 21.
  • the cylindrical support 28 forms for example an enlarged cylindrical base of the fixed cylinder 21, the assembly forming the stator.
  • the stator and rotor assembly is covered with a radome protection not shown.
  • FIGs 6a and 6b illustrate a particular embodiment of the guides and their coupling to the outer cylinder 21 advantageously allowing the minimization of microwave leakage as previously mentioned.
  • the figure 6b is a partial sectional view where the radius of curvature has not been shown for reasons of simplification.
  • the guide emits according to the component E, the radiating opening being made on a small side of the guide.
  • the figure 6b presents a preferred embodiment where the guide 24 and the cavities 52, 53, 53 'are made in the inner cylinder 26.
  • this cylinder may be metallic.
  • the figure 7 specifies, by a partial longitudinal sectional view, an advantageous embodiment where the space 70 between the stator 26 and the rotor 21 is very small, typically having a thickness e typically equal to 0.1 mm with a tolerance of ⁇ 0 , 05 mm.
  • the height of the scanner 1 is for example of the order of 400 mm.
  • the Figures 8a and 8b show an embodiment of the device according to the invention for performing both a conventional radar mode of operation, of the single-stat type, and a bi-static mode of operation.
  • the device comprises two scanners 1, 1 'of the type illustrated by the figures 5a and 5b , the two scanners being connected to the radar 2 according to the figure 8b .
  • the two scanners 1, 1 ' are interconnected by two waveguides 83, 84, a guide 83 connecting the transmission guides 24 of the scanners and the other guide 84 connecting the reception guides 25 of the scanners.
  • the first waveguide 83 is connected via a magic T to the transmission channel 3 connected to the radar.
  • the second waveguide 84 is connected via another magic T to the reception channel 4 connected to the radar.
  • the set of two scanners and the radar is disposed inside a radome 80, of cylindrical shape.
  • the camera 5 is fixed on this radome between the two scanners 1, 1 '.
  • the figure 9 illustrates the two modes of operation of the device illustrated by the Figures 8a and 8b .
  • a single scanner 1 In the single-static mode, a single scanner 1 is used, for transmission to an individual 91 and for reception.
  • the first scanner 1 In the bi-static mode, the first scanner 1 transmits to the individual and the second scanner 1 'realizes the reception of the signals re-transmitted by the individual.
  • the bi-static mode of operation advantageously makes it possible to improve the quality of the radar image.
  • the camera 5 is oriented towards the individual in order to capture the video images thereof.
  • the radar can operate in single-stat mode or bi-static mode.
  • the device according to the invention makes it possible to detect and image magnetic or non-magnetic objects hidden under the clothing of a person who is stationary or in motion.
  • the camera measures the distances on the clothes and, the infrared emission does not penetrate the clothes, allows the formation of a suitable filter in order to obtain a radar imagery of the objects and the determination of their natures, through the clothes .
  • the radar would not allow the measurement of the different distances of the body parts of moving people, because it would be necessary to operate in FMCW mode (frequency-modulated continuous wave) from 70 GHz to 110 GHz to achieve the desired accuracies which are of the order of a millimeter.
  • FMCW mode frequency-modulated continuous wave
  • the two waveguides 3, 4 connect the antenna 1 to the radar 2.
  • a first guide 3 transmits the transmission wave to the antenna.
  • This first waveguide 3 also transmits the reception signals from the antenna to the radar.
  • the second guide 4 transmits the reception wave of the antenna to the radar, via a phase shifter performing a phase rotation of 90 ° on the received signals.
  • the signals are transmitted without phase shift providing the direct component I (t) of the signals received while the second guide 4 provides the quadrature component Q (t).
  • the components thus received are taken into account by the radar reception and processing means 2 for calculating the radar image obtained, this image being of the SAR type as indicated above.
  • the formation of the image Im ( x i , y j ) at a point ( x i , y j ) is effected in a known manner by the integration of the signals received in an analysis time T.
  • L ( x i , y j , t ) is the distance between the radiating source 11, 12 at time t and the point of analysis ( x i , y j ) on the individual, where ⁇ is the length of wave.
  • the distances L ( x i , y j , t ) are delivered by the camera 5.
  • s (t) represents the distance between the center of the transmitting antenna and the camera.
  • the camera makes it possible to produce around the target individual a virtual envelope whose distances to the device according to the invention are known.
  • This virtual envelope corresponds in fact to the outer surface of the clothes worn by the individual. It makes it possible to obtain a reference surface.
  • the measurements made by the camera make it possible to obtain a mesh network representing this surface.
  • the surface can be obtained by smoothing by averaging. This surface is calculated at regular time intervals, for example every 20 ms, to focus on each part of the individual in motion (arms, torso, legs ).
  • the camera which may be of the infrared type, having a retina consisting of a network of CMOS sensors measures the distance by the received power level. For a coding carried out on 12 bits for example, the measurement accuracy can be of 1 millimeter at a distance of one meter.
  • the figure 10 illustrates the detection of an object 103 through a garment 101, the object being fixed on the body 102 of the individual below the garment 101.
  • the distance of the garment is measured and known to the device according to the invention, the garment having been represented as the virtual surface as described above.
  • the obtaining of this envelope is very important because it makes it possible to follow the deformations of the garment due to the body in movement.
  • the camera 5 allows distance measurement according to given periods of time, for example every 20 ms, of all moving parts of the body, more specifically of the clothing envelope. These distance measurements allow the formation of a suitable filter for the formation of images.
  • the imaging process is performed in two steps: an acquisition step and a focusing step.
  • the acquisition step the radar acquires the I and Q components of equation (1) above. Since the radar signals pass through the garments, the acquired image is that of the body possibly equipped with an object 103. The determination of the reflection coefficients of the received signals makes it possible to classically define the nature of the parts of the image and in particular of the object 103.
  • the camera makes it possible to define the distances forming the argument of the exponential of the integral in equation (1) and thus to calculate the image.
  • the resolution of the image is equal to ⁇ . F 2 D .
  • the image obtained is given by relation (1). For each pixel x, y of the image, proceed to the calculation: ⁇ I t + iQ t .
  • the radar 2 transmits at several frequencies, close to a given frequency, for example 77 GHz.
  • the radar 2 emits for example according to five frequencies F1, F2, F3, F4, F5.
  • the pulse is for example divided into five parts, the parts being emitted successively to F1, F2, F3, F4, F5. If the pulse lasts 200 ⁇ s, each part then lasts 40 ⁇ s. More generally, the radar transmits continuously (CW), the emission pulse being divided into N parts, each portion corresponding to a frequency. We remain thereafter in the example where N is equal to 5.
  • the phases and amplitudes are for example calculated for all the frequencies. A first analysis at the first frequency F1 is done on the whole body.
  • measured values of 2.9 and 11 mm respectively of the dielectric permittivity and the thickness for theoretical values of 3.1 and 10 mm can be achieved.
  • the figure 12 shows an exemplary embodiment of a device according to the invention, portable.
  • the antenna part consisting of one or two scanners 1, 1 ', the radar 2 and their interconnection means 3, 4, 83, 84 are arranged inside a cylindrical structure which also acts as a radome 80. structure also supports the camera 5.
  • the structure 80 is connected to a handle 120 for obtaining a portable device, easily manageable and lightweight. Its realization cost may be low because of the type of components used, especially the radar 2 can be a car-type radar, economic, and the camera may be Kinect type, also economic.
  • the components constituting the scanner interior are also economical. This provides a device for detecting illicit objects by detecting forms through clothing and characterizing their material.
  • the detection can easily be done by pointing the device to about one meter from an individual to control.
  • the detection device is connected to viewing means by a suitable wireless link.
  • the visualization means 7 may be a screen disposed in a control center or be within the reach of the user who manipulates the device.
  • the display means may also be glasses worn by the user and on which the detected images are projected. It is possible to provide a second stereoscopic camera to improve the field of view.
  • the figure 13 presents another example of use of a device according to the invention with another "packaging".
  • the control system is here applied at doors 131, 132 opening automatically.
  • Four devices according to the invention two of which are represented by their radomes 80, can be used.
  • a device is placed to the outside and a device is placed inward, each device being placed closer to the opening.
  • an individual or a moving object can be controlled from all angles.
  • a display screen, common to all four devices, is placed at a distance.

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • General Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Radar Systems Or Details Thereof (AREA)

Description

La présente invention concerne un dispositif de détection d'objets portés par un individu, immobile ou en mouvement, ces objets pouvant être des objets illicites cachés sous des vêtements.
La surveillance des personnes dans les lieux publics est devenue une nécessité de sécurité publique. Il existe un besoin croissant de contrôler ce que transportent les individus. Dans la rue, il y a une réelle nécessité de détecter des explosifs, des armes ou encore des drogues. Dans les trains, il faut notamment détecter des explosifs ou des armes. Dans les stades, en plus de ces objets dangereux, il est utile de détecter des bouteilles de verres ou des drogues notamment.
Les solutions de contrôle actuelles sont insuffisantes. Les forces de sécurité disposent :

  • De détecteurs de métaux, qui ne peuvent bien sûr pas détecter les objets non métalliques tels que les explosifs ;
  • De dispositifs à rayons X, utilisables pour des bagages par exemple, mais pas en zone ouverte pour des raisons de santé publique ;
  • D'autorisations de fouilles, mais celles-ci sont lentes et peuvent être contestées.
The present invention relates to a device for detecting objects carried by an individual, immobile or moving, these objects may be illicit objects hidden under clothing.
The surveillance of people in public places has become a necessity of public security. There is a growing need to control what people carry. In the street, there is a real need to detect explosives, weapons or drugs. In trains, you have to detect explosives or weapons. In stadiums, in addition to these dangerous objects, it is useful to detect bottles of glasses or drugs in particular.
Current control solutions are insufficient. Security forces have:
  • Metal detectors, which of course can not detect non-metallic objects such as explosives;
  • X-ray devices, usable for luggage for example, but not in an open area for reasons of public health;
  • Excavation permits, but these are slow and can be challenged.

Les documents FR 3 003 959 A1 et FR 2 844 642 A1 divulguent un système radar équipé d'une antenne rotative à fente hélicoïdale afin de faire de l'imagerie radar pour détecter des objets dangereux portés par un individu. Le document WO 2015/059132 A2 divulgue un radar à ouverture synthétique combiné à une caméra stéréoscopique pour la détection d'objets dangereux portés par un individu. Un but de l'invention est de surmonter ces inconvénients et de permettre la détection d'objets illicites portés par des individus, en mouvement ou immobiles, de façon simple et rapide.
A cet effet, l'invention a pour objet un dispositif de détection d'objets portés par des individus, immobiles ou en mouvement, ledit dispositif comportant au moins :

  • au moins une antenne rotative comportant au moins deux guides d'onde rectilignes parallèles et un cylindre pourvu d'une fente hélicoïdale mobile en rotation autour desdits guides, lesquels sont ouverts en regard de la face intérieure dudit cylindre mobile, ladite surface formant un court-circuit hyperfréquence pour fermer lesdits guides, un desdits guides étant dédié à l'émission, une source rayonnante mobile étant en regard desdits guides par suite du mouvement de rotation dudit cylindre induisant un faisceau d'émission et de réception mobile apte à être orienté vers un individu ;
  • un radar émettant un signal hyperfréquence selon une onde continue (CW) vers le guide d'émission de ladite antenne et recevant les signaux reçus des guides de ladite antenne captés par ledit faisceau mobile, lesdits signaux reçus étant la composante directe I et la composante en quadrature ;
  • une caméra stéréoscopique orientée dans la même direction que ledit faisceau mobile, apte à enregistrer l'enveloppe vestimentaire dudit individu, ladite enveloppe servant de surface de référence pour la mesure des distances audit dispositif ;
  • un calculateur calculant une image de type SAR de la partie du corps dudit individu ciblée par ledit radar et ladite caméra équipé d'éventuels objets, à partir des signaux reçus dudit radar et des distances mesurées par ladite caméra.
The documents FR 3 003 959 A1 and FR 2 844 642 A1 disclose a radar system equipped with a rotating helical slot antenna for radar imaging to detect dangerous objects worn by an individual. The document WO 2015/059132 A2 discloses a synthetic aperture radar combined with a stereoscopic camera for detecting dangerous objects carried by an individual. An object of the invention is to overcome these disadvantages and to allow the detection of illicit objects carried by individuals, moving or immobile, simply and quickly.
To this end, the invention relates to a device for detecting objects carried by individuals, immobile or in motion, said device comprising at least:
  • at least one rotary antenna comprising at least two parallel rectilinear waveguides and a cylinder provided with a helical slot rotatable around said guides, which are open opposite the inner face of said movable cylinder, said surface forming a short microwave circuit for closing said guides, one of said guides being dedicated to the emission, a moving radiating source being opposite to said guides as a result of the rotational movement of said cylinder inducing a mobile transmitting and receiving beam adapted to be directed towards an individual;
  • a radar emitting a microwave signal in a continuous wave (CW) towards the transmission guide of said antenna and receiving the signals received from the guides of said antenna picked up by said moving beam, said received signals being the direct component I and the component in quadrature;
  • a stereoscopic camera oriented in the same direction as said moving beam, able to record the clothing envelope of said individual, said envelope serving as a reference surface for measuring the distances to said device;
  • a calculator calculating a SAR-type image of the part of the body of said individual targeted by said radar and said camera equipped with any objects, from the signals received from said radar and the distances measured by said camera.

Dans un mode de réalisation particulier les deux guides sont gravés dans un cylindre disposé à l'intérieur du cylindre mobile, les deux cylindres ayant le même axe, et l'espace entre les deux cylindres est égal à 0,1 mm ± 0,05 mm.In a particular embodiment, the two guides are engraved in a cylinder disposed inside the mobile cylinder, the two cylinders having the same axis, and the space between the two cylinders is equal to 0.1 mm ± 0.05 mm.

Ladite antenne rotative comporte par exemple un système de minimisation des fuites hyperfréquence, ledit système étant composé de trois cavités, lesdites cavités étant disposées deux à deux de chaque côté desdits guides d'onde, parallèlement à ceux-ci, sur toute leur longueur.Said rotary antenna comprises, for example, a system for minimizing microwave leakage, said system being composed of three cavities, said cavities being arranged in pairs on each side of said waveguides, parallel to these, along their entire length.

Lesdits guides d'onde étant gravés dans un cylindre disposé à l'intérieur du cylindre mobile, ledit cylindre mobile et ledit cylindre intérieur sont par exemple mobiles en rotation par l'intermédiaire d'un dispositif à roulement à billes, la base dudit cylindre mobile et la base dudit cylindre intérieur étant respectivement solidaire mécaniquement de la partie mobile et de la partie fixe dudit dispositif.Said waveguides being engraved in a cylinder disposed inside the mobile cylinder, said mobile cylinder and said inner cylinder are for example rotatable by means of a ball bearing device, the base of said movable cylinder. and the base of said inner cylinder being respectively mechanically secured to the movable part and the fixed part of said device.

Ledit radar fonctionne par exemple dans une bande de fréquence millimétrique.Said radar operates for example in a millimetric frequency band.

Dans un mode de réalisation possible, ledit dispositif comporte deux antennes rotatives pour que ledit radar fonctionne en mode bi-statique, une antenne réalisant l'émission et l'autre antenne étant dédiée à la réception.In one possible embodiment, said device comprises two rotary antennas for said radar to operate in bi-static mode, one antenna transmitting and the other antenna being dedicated to reception.

Dans ce mode de réalisation possible, les antennes sont par exemple reliées entre elles par deux guides d'onde, un guide reliant les guides d'émission desdites antennes et l'autre guide reliant les guides de réception, le premier guide d'onde étant relié via un T magique à un guide d'onde relié au radar et le deuxième guide d'onde étant relié via un autre T magique à un guide d'onde relié au radar.
Ledit radar émet par exemple selon un nombre N de fréquences proches d'une fréquence donnée, l'impulsion d'émission étant découpée en N parties, chaque partie correspondant à une fréquence, un premier niveau d'analyse de l'image étant réalisé pour les signaux reçus à la première desdites fréquences, d'autres analyses étant réalisées pour les signaux reçus aux autres fréquences, les différentes analyses permettant d'approcher la valeur théorique de la permittivité diélectrique d'un objet détecté.
Le calculateur est par exemple partie intégrante des moyens de traitement dudit radar.
Ledit dispositif comportant des moyens de visualisation des images obtenues, lesdits moyens de visualisation sont par exemple des lunettes portées par un utilisateur et sur lesquelles sont projetées lesdites images.
La partie antennaire, le radar et leurs moyens d'interconnexion sont disposés à l'intérieur d'une structure cylindrique portable, faisant également fonction de radôme, ladite structure supportant ladite caméra.
In this possible embodiment, the antennas are for example interconnected by two waveguides, a guide connecting the transmission guides of said antennas and the other guide connecting the reception guides, the first waveguide being connected via a magic T to a waveguide connected to the radar and the second waveguide being connected via another magic T to a waveguide connected to the radar.
Said radar emits, for example, according to a number N of frequencies close to a given frequency, the emission pulse being divided into N parts, each part corresponding to a frequency, a first level of analysis of the image being carried out for the signals received at the first of said frequencies, other analyzes being carried out for the signals received at the other frequencies, the various analyzes making it possible to approach the theoretical value of the dielectric permittivity of a detected object.
The computer is for example an integral part of the processing means of said radar.
Said device comprising means for displaying the images obtained, said viewing means are for example glasses worn by a user and on which said images are projected.
The antenna part, the radar and their interconnection means are arranged inside a portable cylindrical structure, also acting as a radome, said structure supporting said camera.

D'autres caractéristiques et avantages de l'invention apparaîtront à l'aide de la description qui suit, faite en regard de dessins annexés qui représentent :

  • La figure 1, les principaux composants formant un dispositif selon l'invention ;
  • Les figures 2a et 2b, le principe de réalisation de l'antenne rotative utilisée dans le dispositif selon l'invention ;
  • La figure 3, une vue transversale de ladite antenne ;
  • Les figures 4a à 4e, une illustration du fonctionnement de ladite antenne ;
  • Les figures 5a et 5b, un exemple de réalisation de ladite antenne ;
  • Les figures 6a et 6b, un exemple de réalisation permettant de minimiser les fuites hyperfréquence au niveau de ladite antenne ;
  • La figure 7, une vue en coupe longitudinale de ladite antenne ;
  • Les figures 8a et 8b, un exemple de réalisation d'un dispositif selon l'invention permettant un fonctionnement de type bi-statique ;
  • La figure 9, une illustration du fonctionnement mono-statique et une illustration du fonctionnement bi-statique ;
  • La figure 10, une illustration de la détection d'un objet à travers un vêtement ;
  • La figure 11, une zone détection soumise à l'analyse d'un signal multifréquences ;
  • La figure 12, un exemple de réalisation d'un dispositif selon l'invention, portable ;
  • La figure 13, un exemple d'application de dispositifs selon l'invention équipant des portes pour le contrôle d'un passage.
Other characteristics and advantages of the invention will become apparent with the aid of the description which follows, given with regard to appended drawings which represent:
  • The figure 1 the main components forming a device according to the invention;
  • The Figures 2a and 2b , the principle of realization of the rotary antenna used in the device according to the invention;
  • The figure 3 a transverse view of said antenna;
  • The Figures 4a to 4e an illustration of the operation of said antenna;
  • The figures 5a and 5b an embodiment of said antenna;
  • The Figures 6a and 6b an exemplary embodiment for minimizing microwave leakage at said antenna;
  • The figure 7 a longitudinal sectional view of said antenna;
  • The Figures 8a and 8b , an exemplary embodiment of a device according to the invention for a bi-static type operation;
  • The figure 9 , an illustration of the mono-static operation and an illustration of the bi-static operation;
  • The figure 10 , an illustration of the detection of an object through a garment;
  • The figure 11 a detection zone subjected to the analysis of a multifrequency signal;
  • The figure 12 , an exemplary embodiment of a device according to the invention, portable;
  • The figure 13 , an example of application of devices according to the invention equipping doors for the control of a passage.

La figure 1 illustre les principaux composants formant un dispositif selon l'invention. Il comporte au moins :

  • une antenne rotative 1 dont le fonctionnement sera décrit par la suite et que l'on pourra appeler également scanner ;
  • un radar 2, à onde continue (CW) fonctionnant par exemple à une fréquence centrale proche de 77 GHz, à faible coût fonctionnant en mode de réception homodyne, et comportant notamment la génération des ondes d'émission à la fréquence centrale, les moyens de réception et les moyens d'émission, le radar 2 fournissant une image radar à partir des signaux reçus par l'antenne rotative selon le principe de l'imagerie SAR comme cela sera décrit par la suite ;
  • deux guides d'onde 3, 4 assurant pour l'un la transmission des signaux hyperfréquences du radar 2 vers l'antenne 1 et pour l'autre de l'antenne vers le radar ;
  • une caméra stéréoscopique 5, par exemple de type Kinect ;
  • un calculateur 6 combinant l'image obtenue par la caméra avec l'image obtenue par le radar afin de visualiser les éventuels objets détectés en superposition de l'image stéréoscopique obtenue par la caméra ;
  • un écran 7 ou tout autre moyen de visualisation, reliée au calculateur, affichant l'image finale.
The figure 1 illustrates the main components forming a device according to the invention. It includes at least:
  • a rotary antenna 1 whose operation will be described later and that we can also call scanner;
  • a continuous-wave (CW) radar 2 operating, for example, at a central frequency close to 77 GHz, at low cost operating in homodyne reception mode, and comprising in particular the generation of transmission waves at the central frequency, the means of reception and transmission means, the radar 2 providing a radar image from the signals received by the rotating antenna according to the principle of SAR imaging as will be described later;
  • two waveguides 3, 4 ensuring for one the transmission of the microwave signals from the radar 2 to the antenna 1 and the other from the antenna to the radar;
  • a stereoscopic camera 5, for example of the Kinect type;
  • a calculator 6 combining the image obtained by the camera with the image obtained by the radar in order to visualize any detected objects superimposed on the stereoscopic image obtained by the camera;
  • a screen 7 or any other visualization means, connected to the computer, displaying the final image.

On va décrire par la suite les différents composants du dispositif selon l'invention.The various components of the device according to the invention will be described later.

Les figures 2a et 2b illustrent le principe de réalisation possible du scanner 1. La figure 2 illustre le principe de réalisation. L'antenne 1 comporte un cylindre métallique 21 présentant une ouverture rayonnante 22 suivant une ligne hélicoïdale 23 parcourant le tour du cylindre. L'antenne comporte au moins une paire de guides d'onde 24, 25 disposés à l'intérieur du cylindre et ouverts vers la paroi intérieure du cylindre. Un guide d'onde 24 est réservé à l'émission et l'autre guide d'onde 25 est réservé à la réception. Le guide d'émission 24 est relié aux moyens d'émission du radar 2 et le guide de réception 25 est relié aux moyens de réception du radar 2. Le cylindre 21 et les guides d'ondes 24, 25 ont un mouvement de rotation relatif par rapport à l'axe 100 du cylindre.
De préférence, les guides restent fixes et le cylindre 21 est animé d'un mouvement de rotation autour des guides. Les guides 24, 25 sont placés sur un support 26 disposé à l'intérieur du cylindre 21.
The Figures 2a and 2b illustrate the principle of possible realization of the scanner 1. The figure 2 illustrates the principle of realization. The antenna 1 comprises a metal cylinder 21 having a radiating opening 22 in a helical line 23 running around the cylinder. The antenna comprises at least one pair of waveguides 24, 25 disposed inside the cylinder and open towards the inner wall of the cylinder. A waveguide 24 is reserved for transmission and the other waveguide 25 is reserved for reception. The transmission guide 24 is connected to the transmitting means of the radar 2 and the reception guide 25 is connected to the reception means of the radar 2. The cylinder 21 and the waveguides 24, 25 have a relative rotational movement relative to the axis 100 of the cylinder.
Preferably, the guides remain fixed and the cylinder 21 is rotated around the guides. The guides 24, 25 are placed on a support 26 disposed inside the cylinder 21.

La figure 2b illustre un exemple de réalisation du support 26 des guides d'onde 24, 25. Ce support 26, disposé à l'intérieur du premier cylindre 21, est un cylindre. Il forme le stator dans le cas où le premier cylindre 21, le rotor, est animé d'un mouvement de rotation. Les guides d'onde 24, 25 sont disposés sur le cylindre intérieur 26. Dans un mode de réalisation préféré, les guides 24, 25 sont gravés dans ce cylindre 26. En effet, compte-tenu de la vitesse de déplacement des personnes à surveiller, allant de 0,5 à 3 km/h, pour obtenir un bon échantillonnage de l'antenne synthétique, à 0,5 λ (λ étant la longueur de l'onde hyperfréquence utilisée), la vitesse de rotation du rotor doit être comprise entre 1500 et 3000 tours par minute, ce qui exclut toute asymétrie du stator. Cela impose un stator avec une enveloppe extérieure cylindrique, et donc des guides d'onde gravés dans le cylindre.
L'antenne 1 comporte deux guides 24, 25, l'un en émission et l'autre en réception, ces deux guides distincts permettant avantageusement une auto calibration en temps réel. En effet, tout système mécanique fonctionnant aux vitesses de rotation telles que celle annoncée précédemment nécessite un système de calibration quasiment en temps réel. Cette calibration nécessite la mesure des différents trajets hyperfréquence à l'intérieur du dispositif qui peut être avantageusement réalisée par le couplage externe entre l'émission produite par le guide d'émission 24 et la réception sur l'autre guide 25, permettant ainsi des actions préventives contre des dérèglements.
The figure 2b illustrates an exemplary embodiment of the support 26 of the waveguides 24, 25. This support 26, disposed inside the first cylinder 21, is a cylinder. It forms the stator in the case where the first cylinder 21, the rotor, is driven by a rotational movement. The waveguides 24, 25 are arranged on the inner cylinder 26. In a preferred embodiment, the guides 24, 25 are etched in this cylinder 26. In fact, given the speed of movement of the people to be monitored , from 0.5 to 3 km / h, to obtain a good sampling of the synthetic antenna, at 0.5 λ (λ being the length of the microwave wave used), the speed of rotation of the rotor must be understood between 1500 and 3000 revolutions per minute, which excludes any asymmetry of the stator. This imposes a stator with a cylindrical outer envelope, and thus waveguides etched in the cylinder.
The antenna 1 comprises two guides 24, 25, one in transmission and the other in reception, these two distinct guides advantageously allowing a car real-time calibration. Indeed, any mechanical system operating at rotation speeds such as that previously announced requires a calibration system almost in real time. This calibration requires the measurement of the different microwave paths inside the device which can be advantageously achieved by the external coupling between the emission produced by the transmission guide 24 and the reception on the other guide 25, thus enabling actions preventative measures against disturbances.

La figure 3 présente par une vue transversale la disposition du cylindre intérieur 26 par rapport au cylindre extérieur 21, les deux cylindres ayant le même axe de symétrie 100. Le diamètre du cylindre intérieur 26 est par exemple défini de façon à ce que la face rayonnante des guides soit à une distance donnée du cylindre extérieur que l'on précisera par la suite. Lorsque la face rayonnante est en regard de la partie métallisée intérieure du cylindre, et non de l'ouverture, cette face métallisée joue le rôle d'un court circuit hyperfréquence, sans pour autant éviter les fuites au niveau des contacts. Pour éviter ces fuites importantes, on dispose le long des guides d'onde d'émission et de réception 24, 25 trois fentes gravées dans le cylindre intérieur jouant le rôle de courts circuits permettant de ramener des courts circuits au niveau des guides. Un exemple de réalisation de ces fentes sera présenté aux figures 6a et 6b.
Le principe de réalisation de l'antenne rotative illustré par les figures 2a, 2b et 3 utilise une paire de guides d'onde 24, 25, l'un pour l'émission et l'autre pour la réception. Il est possible de prévoir un mode de réalisation comportant deux paires de guides d'ondes (émission et réception). Dans ce cas, la deuxième paire est par exemple diamétralement opposée à la première paire 24, 25. Les deux paires de guides sont alors par exemple reliées au radar 2 via un commutateur SP4T. Avantageusement, une telle antenne permet d'augmenter le domaine de contrôle.
The figure 3 presents by a transverse view the arrangement of the inner cylinder 26 with respect to the outer cylinder 21, the two cylinders having the same axis of symmetry 100. The diameter of the inner cylinder 26 is for example defined so that the radiating face of the guides is at a given distance from the outer cylinder that will be specified later. When the radiating face is facing the inner metallized portion of the cylinder, and not the opening, this metallized face acts as a short microwave circuit, without preventing leaks at the contacts. In order to avoid these large leaks, along the emission and reception waveguides 24, three slots are provided, engraved in the inner cylinder acting as short circuits making it possible to reduce short circuits to the level of the guides. An example of realization of these slots will be presented to Figures 6a and 6b .
The principle of realization of the rotary antenna illustrated by the Figures 2a, 2b and 3 uses a pair of waveguides 24, 25, one for transmission and the other for reception. It is possible to provide an embodiment comprising two pairs of waveguides (transmission and reception). In this case, the second pair is for example diametrically opposed to the first pair 24, 25. The two pairs of guides are then for example connected to the radar 2 via an SP4T switch. Advantageously, such an antenna makes it possible to increase the control domain.

Les figures 4a, 4b, 4c, 4d et 4e illustrent le fonctionnement d'une antenne telle que décrite précédemment, plus particulièrement le mode détection qu'elle permet. Les figures 4a et 4b représentent une vue en coupe partielle, selon l'axe 100, de deux positions relatives des cylindres 21, 26. Les figures 4c et 4d illustrent respectivement les positions relatives des deux cylindres des vues partielles des figures 4a et 4b par des vues de dessus. Ces figures montrent qu'en présence du cylindre extérieur 26, les fentes 24, 25 forment deux guides d'onde hyperfréquence sans contact, la rotation du cylindre intérieur 26 en regard du cylindre extérieur fixe et ouvert longitudinalement formant deux sources rayonnantes mobiles.
Pour faciliter l'explication de ce phénomène, on considère un seul faisceau, correspondant par exemple au guide d'onde en émission 24. En fonctionnement, les parties du guide 24 qui font face à la paroi métallisée du cylindre 21 ne rayonnent pas. Les parties du guide qui sont en regard de l'ouverture 22 participent au rayonnement de l'antenne, en émission et en réception. En fait, en raison de la forme hélicoïdale du guide d'onde 25 suivant une hélice et de sa rotation par rapport l'ouverture 22 longitudinale du cylindre fixe, le guide 24 se présente en regard de l'ouverture comme un élément de guide glissant effectuant des allers et retours rectilignes.
La figure 4a illustre la position d'une partie du guide 24 au regard de l'ouverture rayonnante à un instant donné t0. La figure 4e illustre le faisceau d'antenne F1 associé à la position de la figure 4a avec son centre de phase 41 situé au niveau de la partie guide 24 formant illuminateur ou source rayonnante. Le faisceau F1 représente ici la couverture angulaire de l'antenne. La figure 4b illustre les mêmes éléments que ceux de la figure 4a, mais à un instant suivant t0 + Δt. Dans le plan de la figure, la partie du guide 24 formant source rayonnante, en regard de l'ouverture 22, s'est alors décalée d'une distance Δ par suite de la rotation du cylindre intérieur 26. Le faisceau d'antenne F1 correspondant à la position de cylindre intérieur 26 de
la figure 4b est représenté avec son centre de phase 42 qui s'est décalé d'une distance Δ. La rotation du cylindre intérieur supportant le guide 24 permet donc le déplacement continu du centre de phase du rayonnement et donc du faisceau F1. Le long de l'axe 43 de l'ouverture longitudinale 22, parallèle à l'axe 100 du cylindre, le centre de phase se déplace entre une position x0 - ΔMax/2 et x0 + ΔMax/2. L'amplitude du déplacement ΔMax dépend du pas de l'hélice 23 que suit l'ouverture rayonnante. La vitesse de rotation du cylindre intérieur 26 est telle que le centre de phase 41, 42 se déplace linéairement à une vitesse qui peut atteindre 30 m/s.
La largeur du faisceau F1 est fonction de la largeur d de l'ouverture 22 du cylindre extérieur, formant ouverture rayonnante. Plus d est petite, plus le faisceau d'antenne est large. La largeur à 3dB du faisceau F1 est λ/d, où λ est la longueur d'onde émise. Le principe de balayage est le même en réception avec le guide de réception 25.
La rotation du cylindre intérieur permet donc le déplacement continu du centre de phase du rayonnement, et permet ainsi d'obtenir un fonctionnement du type radar à antenne synthétique ou SAR. Cette propriété est par les moyens de traitement du radar 2 pour obtenir et analyser des images radar à haute résolution. Pour mémoire, les radars à antenne synthétique sont des radars dont l'antenne est orientée perpendiculairement à la route du porteur. C'est le porteur du radar, et plus particulièrement de l'antenne, qui dans son déplacement engendre l'observation de l'espace. Dans le cas présent, le déplacement du porteur est simulé par le déplacement du centre de phase. Les deux dimensions de l'image radar sont définies par la direction de propagation et le déplacement du porteur. La résolution spatiale, qui conditionne la finesse de l'image observée, est donc obtenue :

  • dans la direction perpendiculaire au mouvement du porteur par la résolution en distance du radar ;
  • dans la direction du mouvement du porteur par la largeur du faisceau F1.
Le traitement du type SAR est notamment décrit dans l'ouvrage de J.Darricau : Physique et Théorie du Radar -Tome 3, 3ème édition - Chapitre 21, page 483 - Editeur Sodipe, Paris 1994 .
Un ensemble de récepteurs disposés le long de l'axe 43 est alors reconstitué dans le temps comme dans une application de type SAR, permettant ainsi de réaliser des images radar. En effet, à partir des coefficients de réflexion mesurés pour chaque pixel de l'image on reconstitue la forme des objets.The Figures 4a, 4b , 4c, 4d and 4th illustrate the operation of an antenna as described above, more particularly the detection mode that it allows. The Figures 4a and 4b represent a partial sectional view, along the axis 100, of two relative positions of the cylinders 21, 26. Figures 4c and 4d respectively illustrate the relative positions of the two cylinders partial views of Figures 4a and 4b by views from above. These figures show that in the presence of the outer cylinder 26, the slots 24, 25 form two non-contact microwave waveguides, the rotation of the inner cylinder 26 opposite the fixed outer cylinder and open longitudinally forming two mobile radiating sources.
To facilitate the explanation of this phenomenon, consider a single beam, corresponding for example to the emission waveguide 24. In operation, the portions of the guide 24 which face the metallized wall of the cylinder 21 do not radiate. The portions of the guide which are opposite the opening 22 participate in the radiation of the antenna, transmission and reception. In fact, because of the helical shape of the waveguide 25 in a helix and its rotation relative to the longitudinal opening 22 of the fixed cylinder, the guide 24 is presented opposite the opening as a sliding guide element. making straight round trips.
The figure 4a illustrates the position of a portion of the guide 24 with respect to the opening radiating at a given instant t 0 . The figure 4e illustrates the antenna beam F 1 associated with the position of the figure 4a with its phase center 41 located at the guide portion 24 forming an illuminator or radiating source. The beam F 1 here represents the angular coverage of the antenna. The figure 4b illustrates the same elements as those of the figure 4a , but at a time following t 0 + Δt. In the plane of the figure, the portion of the guide 24 radiating source, opposite the opening 22, then shifted by a distance Δ due to the rotation of the inner cylinder 26. The antenna beam F 1 corresponding to the inner cylinder position 26 of
the figure 4b is represented with its phase center 42 which has shifted by a distance Δ. The rotation of the inner cylinder supporting the guide 24 thus allows the continuous displacement of the phase center of the radiation and thus of the beam F 1 . Along the axis 43 of the longitudinal opening 22, parallel to the axis 100 of the cylinder, the phase center moves between a position x 0 - Δ Max / 2 and x 0 + Δ Max / 2. The amplitude of displacement Δ Max depends on the pitch of the helix 23 that follows the radiating opening. The rotational speed of the inner cylinder 26 is such that the phase center 41, 42 moves linearly at a speed of up to 30 m / s.
The width of the beam F 1 is a function of the width d of the opening 22 of the outer cylinder, forming a radiating opening. More is small, the more Antenna beam is wide. The width at 3dB of the beam F 1 is λ / d, where λ is the wavelength emitted. The scanning principle is the same in reception with the reception guide 25.
The rotation of the inner cylinder thus allows the continuous displacement of the phase center of the radiation, and thus makes it possible to obtain a synthetic antenna or SAR type radar operation. This property is by the radar processing means 2 to obtain and analyze high resolution radar images. For the record, synthetic antenna radars are radars whose antenna is oriented perpendicular to the carrier's road. It is the carrier of the radar, and more particularly of the antenna, which in its displacement generates the observation of the space. In this case, the movement of the carrier is simulated by the displacement of the phase center. The two dimensions of the radar image are defined by the direction of propagation and the movement of the carrier. The spatial resolution, which conditions the fineness of the image observed, is thus obtained:
  • in the direction perpendicular to the movement of the carrier by the distance resolution of the radar;
  • in the direction of the movement of the carrier by the width of the beam F1.
The SAR type processing is described in particular in J.Darricau: Physics and Radar Theory -Tome 3, 3rd edition - Chapter 21, page 483 - Publisher Sodipe, Paris 1994 .
A set of receivers arranged along the axis 43 is then reconstituted in time as in a SAR-type application, thus making it possible to produce radar images. Indeed, from the reflection coefficients measured for each pixel of the image is reconstructed the shape of the objects.

Dans le mode de réalisation décrit par les figures 2a et 2b, le cylindre intérieur 26 comportant les deux guides d'onde 24, 25 est fixe, les deux guides étant rectilignes. Le rotor 21 comporte la fente hélicoïdale 22 qui tourne autour des guides.
Il est possible de prévoir un mode de réalisation où le cylindre intérieur 26 équipé des guides d'onde tourne, formant rotor, alors que la fente hélicoïdale 22 reste fixe.
In the embodiment described by the Figures 2a and 2b , the inner cylinder 26 comprising the two waveguides 24, 25 is fixed, the two guides being rectilinear. The rotor 21 has the helical slot 22 which rotates around the guides.
It is possible to provide an embodiment where the inner cylinder 26 equipped with rotating waveguides, forming a rotor, while the helical slot 22 remains fixed.

Dans un autre mode de réalisation les guides d'onde ont une forme hélicoïdale et la fente en rotation autour des guides est rectiligne. Ce mouvement de rotation est relatif, c'est-à-dire que soit les fentes peuvent être fixes et la fente mobile en rotation, ou à l'inverse les guides sont mobiles en rotation et la fente est fixe.
Lorsque le cylindre creux portant la fente est fixe, celui-ci peut faire office de radôme, évitant également que la fente se déforme sous l'effet de la rotation. Des guides d'onde en rotation nécessitent cependant un système de joint tournant et un mécanisme adapté pour échanger les signaux avec le radar. Pour tous ces modes de réalisation, le principe de fonctionnement reste celui décrit aux figures 4a à 4e. Par la suite, on considère un mode de réalisation selon les figures 2a et 2b où les guides restent fixes.
In another embodiment, the waveguides have a helical shape and the slot in rotation around the guides is rectilinear. This rotational movement is relative, that is to say either the slots can be fixed and the slot rotatable, or conversely the guides are rotatable and the slot is fixed.
When the hollow cylinder carrying the slot is fixed, it can act as a radome, also avoiding that the slot deforms under the effect of rotation. Rotating waveguides, however, require a rotating joint system and a mechanism adapted to exchange the signals with the radar. For all these embodiments, the operating principle remains that described in Figures 4a to 4e . Subsequently, an embodiment according to the Figures 2a and 2b where the guides remain fixed.

Les figures 5a et 5b présente un exemple de réalisation conforme à ce mode de réalisation, la figure 5a représentant le cylindre intérieur fixe 26, stator, équipé des deux guides d'onde 24, 25 et la figure 5b représentant le cylindre extérieur 21, équipé de la fente hélicoïdale, en rotation autour du cylindre fixe.
Le cylindre extérieur 21 est entraîné en rotation par un moteur 19, représenté en figure 1. Il glisse en rotation par rapport à la partie fixe via un dispositif à roulement à billes cylindrique 30. La partie fixe 27 du roulement à billes est solidaire mécaniquement de la base du cylindre intérieur 26 et la partie mobile 27' du roulement à billes est solidaire mécaniquement d'un support 28, par exemple de forme cylindrique, ce support étant lui-même solidaire mécaniquement du cylindre extérieur 21. Le support cylindrique 28 forme par exemple une embase cylindrique élargie du cylindre fixe 21, l'ensemble formant le stator.
L'ensemble stator et rotor est recouvert d'un radôme de protection non représenté.
The figures 5a and 5b presents an exemplary embodiment according to this embodiment, the figure 5a representing the fixed inner cylinder 26, stator, equipped with two waveguides 24, 25 and the figure 5b representing the outer cylinder 21, equipped with the helical slot, rotating around the fixed cylinder.
The outer cylinder 21 is rotated by a motor 19, shown in FIG. figure 1 . It slides in rotation relative to the fixed portion via a cylindrical ball bearing device 30. The fixed portion 27 of the ball bearing is mechanically secured to the base of the inner cylinder 26 and the movable portion 27 'of the ball bearing is secured to mechanically of a support 28, for example of cylindrical shape, this support being itself mechanically secured to the outer cylinder 21. The cylindrical support 28 forms for example an enlarged cylindrical base of the fixed cylinder 21, the assembly forming the stator.
The stator and rotor assembly is covered with a radome protection not shown.

Les figures 6a et 6b illustrent un mode particulier de réalisation des guides et leur couplage au cylindre extérieur 21 permettant avantageusement la minimisation des fuites hyperfréquence comme cela a été évoqué précédemment. La figure 6b est une vue en coupe partielle où le rayon de courbure n'a pas été représenté pour des raisons de simplification.The Figures 6a and 6b illustrate a particular embodiment of the guides and their coupling to the outer cylinder 21 advantageously allowing the minimization of microwave leakage as previously mentioned. The figure 6b is a partial sectional view where the radius of curvature has not been shown for reasons of simplification.

La figures 6a présente, par une vue partielle en perspective, la réalisation d'un guide, à titre d'exemple on considère le guide d'émission 24. Le guide de réception 25 est réalisé et couplé de la même façon.
Le guide d'onde 24 est un guide à section rectangulaire comportant une ouverture rayonnante 51. La face intérieure métallisée du cylindre extérieur 21 forme un court-circuit pour fermer le guide. La rotation du guide 24 à l'intérieur de ce cylindre 21 a pour effet de créer une source rayonnante qui se déplace le long de son ouverture longitudinale 22. Le guide d'onde 24 est relié par une extrémité aux circuits d'émission du radar 2 et autres circuits par des moyens de transmission qui seront décrits par la suite. Il est relié à son autre extrémité à une charge adaptée.
Deux cavités 52, 53 parallèles sont réalisées de chaque côté du guide 24, sur toute sa longueur. Ces cavités étant parallèles au guide d'onde 24, elles suivent également la ligne hélicoïdale 23.
La figure 6b présente les deux guides d'onde 24, 25 entourés chacun d'une cavité. Le guide d'onde d'émission 24 est entouré à gauche d'une cavité 53 et à droite d'une cavité 52. Le guide d'onde de réception 25 est entouré à gauche de cette dernière cavité 52, commune aux deux guides, et à droite par une cavité 53'.
Les ouvertures 54, 55, 54' des cavités sont sensiblement dans le plan de l'ouverture 51 du guide, plus précisément dans une même ligne de courbure.
Avantageusement, ces cavités piègent les ondes hyperfréquence et limitent très fortement, voire suppriment les fuites hyperfréquences.
Ces cavités 52, 53, 53' sont moins larges et moins profondes que le guide. Les dimensions sont par exemple les suivantes, λ étant la longueur d'onde émise, correspondant à la fréquence centrale :

  • Profondeur d'un guide 24, 25 : 0,75 À ;
  • Largeur d'un guide 24, 25 : 0,35 À ;
  • Profondeur d'une cavité latérale 52, 53, 53' : 0,25 λ ;
  • Largeur d'une cavité latérale 52, 53, 53' : 0,12 λ ;
La distance entre l'ouverture 51 du guide et les ouvertures 54, 55, 54' des cavités d'une part et la face intérieure du cylindre 21 peut aller de 0,1 λ à 2 λ. Dans le cas d'application avec le radar 2 fonctionnant à 77 GHz, λ est de l'ordre de quelques millimètres.The Figures 6a presents, by a partial perspective view, the production of a guide, for example, the transmission guide 24 is considered. The reception guide 25 is produced and coupled in the same way.
The waveguide 24 is a rectangular section guide having a radiating aperture 51. The metallized inner face of the outer cylinder 21 forms a short circuit to close the guide. The rotation of the guide 24 inside this cylinder 21 has the effect of creating a radiating source which moves along its longitudinal opening 22. The waveguide 24 is connected at one end to the radar transmission circuits. 2 and other circuits by transmission means which will be described later. It is connected at its other end to a suitable load.
Two parallel cavities 52, 53 are formed on each side of the guide 24, over its entire length. These cavities being parallel to the waveguide 24, they also follow the helical line 23.
The figure 6b presents the two waveguides 24, 25 each surrounded by a cavity. The emission waveguide 24 is surrounded on the left by a cavity 53 and on the right by a cavity 52. The reception waveguide 25 is surrounded to the left of this latter cavity 52, common to both guides. and on the right by a cavity 53 '.
The openings 54, 55, 54 'of the cavities are substantially in the plane of the opening 51 of the guide, more precisely in the same line of curvature.
Advantageously, these cavities trap the microwave waves and very strongly limit or even eliminate microwave leakage.
These cavities 52, 53, 53 'are less wide and shallower than the guide. The dimensions are for example the following, where λ is the emitted wavelength, corresponding to the central frequency:
  • Depth of a guide 24, 25: 0.75 Å;
  • Width of a guide 24, 25: 0.35 Å;
  • Depth of a lateral cavity 52, 53, 53 ': 0.25 λ;
  • Width of a lateral cavity 52, 53, 53 ': 0.12 λ;
The distance between the opening 51 of the guide and the openings 54, 55, 54 'of the cavities on the one hand and the inner face of the cylinder 21 can range from 0.1λ to 2λ. In the case of application with the radar 2 operating at 77 GHz, λ is of the order of a few millimeters.

Dans l'exemple des figures 6a et 6b, le guide émet selon la composante E, l'ouverture rayonnante étant réalisée sur un petit côté du guide.
La figure 6b présente un mode de réalisation préférentiel où le guide 24 et les cavités 52, 53, 53' sont réalisés dans le cylindre intérieur 26. A cet effet, ce cylindre peut être métallique. Comme pour les guides d'onde 24, 25, les cavités 52, 53, 53' peuvent être gravées dans le cylindre.
In the example of Figures 6a and 6b , the guide emits according to the component E, the radiating opening being made on a small side of the guide.
The figure 6b presents a preferred embodiment where the guide 24 and the cavities 52, 53, 53 'are made in the inner cylinder 26. For this purpose, this cylinder may be metallic. As for the waveguides 24, 25, the cavities 52, 53, 53 'can be etched in the cylinder.

La figure 7 précise, par une vue en coupe longitudinale partielle, un mode de réalisation avantageux où l'espace 70 entre le stator 26 et le rotor 21 est très faible, ayant typiquement une épaisseur e typiquement égale à 0,1 mm avec une tolérance de ± 0,05 mm.
La hauteur du scanner 1 est par exemple de l'ordre de 400 mm.
The figure 7 specifies, by a partial longitudinal sectional view, an advantageous embodiment where the space 70 between the stator 26 and the rotor 21 is very small, typically having a thickness e typically equal to 0.1 mm with a tolerance of ± 0 , 05 mm.
The height of the scanner 1 is for example of the order of 400 mm.

Les figures 8a et 8b présentent un mode de réalisation du dispositif selon l'invention permettant de faire à la fois un mode de fonctionnement radar classique, de type mono-statique, et un mode de fonctionnement bi-statique.
A cet effet, le dispositif comporte deux scanners 1, 1' du type de celui illustré par les figures 5a et 5b, les deux scanners étant reliés au radar 2 conformément à la figure 8b. Les deux scanners 1, 1' sont reliés entre eux par deux guides d'onde 83, 84, un guide 83 reliant les guides d'émission 24 des scanners et l'autre guide 84 reliant les guides de réception 25 des scanners.
Le premier guide d'onde 83 est relié via un T magique à la voie d'émission 3 reliée au radar. Le deuxième guide d'onde 84 est relié via un autre T magique à la voie de réception 4 reliée au radar.
L'ensemble des deux scanners et du radar est disposé à l'intérieur d'un radôme 80, de forme cylindrique. La caméra 5 est fixée sur ce radôme entre les deux scanners 1, 1'.
The Figures 8a and 8b show an embodiment of the device according to the invention for performing both a conventional radar mode of operation, of the single-stat type, and a bi-static mode of operation.
For this purpose, the device comprises two scanners 1, 1 'of the type illustrated by the figures 5a and 5b , the two scanners being connected to the radar 2 according to the figure 8b . The two scanners 1, 1 'are interconnected by two waveguides 83, 84, a guide 83 connecting the transmission guides 24 of the scanners and the other guide 84 connecting the reception guides 25 of the scanners.
The first waveguide 83 is connected via a magic T to the transmission channel 3 connected to the radar. The second waveguide 84 is connected via another magic T to the reception channel 4 connected to the radar.
The set of two scanners and the radar is disposed inside a radome 80, of cylindrical shape. The camera 5 is fixed on this radome between the two scanners 1, 1 '.

La figure 9 illustre les deux modes de fonctionnement du dispositif illustré par les figures 8a et 8b. Dans le mode mono-statique, un seul scanner 1 est utilisé, pour l'émission vers un individu 91 et pour la réception. Dans le mode bi-statique, le premier scanner 1 effectue l'émission vers l'individu et le deuxième scanner 1' réalise la réception des signaux réémis par l'individu.The figure 9 illustrates the two modes of operation of the device illustrated by the Figures 8a and 8b . In the single-static mode, a single scanner 1 is used, for transmission to an individual 91 and for reception. In the bi-static mode, the first scanner 1 transmits to the individual and the second scanner 1 'realizes the reception of the signals re-transmitted by the individual.

Le mode de fonctionnement bi-statique permet avantageusement d'améliorer la qualité de l'image radar. La caméra 5 est orientée vers l'individu afin de capter les images vidéo de celui-ci.The bi-static mode of operation advantageously makes it possible to improve the quality of the radar image. The camera 5 is oriented towards the individual in order to capture the video images thereof.

On revient à la figure 1, pour décrire la formation des images radar en combinaison avec la caméra stéréoscopique 5. Le radar peut fonctionner en mode mono-statique ou en mode bi-statique.
Le dispositif selon l'invention permet de détecter et d'imager des objets magnétiques ou non magnétiques cachés sous les vêtements d'une personne fixe ou en mouvement.
Avantageusement, la caméra mesure les distances sur les vêtements et, l'émission infrarouge ne pénétrant pas les vêtements, permet la formation d'un filtre adapté afin d'obtenir une imagerie radar des objets et la détermination de leurs natures, à travers les vêtements.
Il est à noter qu'en l'absence de cette caméra, le radar ne permettrait pas la mesure des différentes distances des parties du corps des personnes en mouvement, car il serait nécessaire d'opérer en mode FMCW (onde continue modulée en fréquence) de 70 GHz à 110 GHz pour atteindre les précisions recherchées qui sont de l'ordre du millimètre.
We come back to figure 1 , to describe the formation of the radar images in combination with the stereoscopic camera 5. The radar can operate in single-stat mode or bi-static mode.
The device according to the invention makes it possible to detect and image magnetic or non-magnetic objects hidden under the clothing of a person who is stationary or in motion.
Advantageously, the camera measures the distances on the clothes and, the infrared emission does not penetrate the clothes, allows the formation of a suitable filter in order to obtain a radar imagery of the objects and the determination of their natures, through the clothes .
It should be noted that in the absence of this camera, the radar would not allow the measurement of the different distances of the body parts of moving people, because it would be necessary to operate in FMCW mode (frequency-modulated continuous wave) from 70 GHz to 110 GHz to achieve the desired accuracies which are of the order of a millimeter.

Les deux guides d'onde 3, 4 relient l'antenne 1 au radar 2. Un premier guide 3 transmet l'onde d'émission vers l'antenne. Ce premier guide d'onde 3 transmet également les signaux de réception de l'antenne vers le radar. Le deuxième guide 4 transmet l'onde de réception de l'antenne vers le radar, via un déphaseur effectuant une rotation de phase de 90° sur les signaux reçus.
Ainsi par la voie directe, utilisant le premier guide 3, on transmet les signaux sans déphasage fournissant la composante directe I(t) des signaux reçus alors que le deuxième guide 4 fournit la composante en quadrature Q(t).
Les composantes ainsi reçues sont prises en compte par les moyens de réception et de traitement du radar 2 pour le calcul de l'image radar obtenue, cette image étant de type SAR comme indiqué précédemment.
The two waveguides 3, 4 connect the antenna 1 to the radar 2. A first guide 3 transmits the transmission wave to the antenna. This first waveguide 3 also transmits the reception signals from the antenna to the radar. The second guide 4 transmits the reception wave of the antenna to the radar, via a phase shifter performing a phase rotation of 90 ° on the received signals.
Thus, in the direct way, using the first guide 3, the signals are transmitted without phase shift providing the direct component I (t) of the signals received while the second guide 4 provides the quadrature component Q (t).
The components thus received are taken into account by the radar reception and processing means 2 for calculating the radar image obtained, this image being of the SAR type as indicated above.

La formation de l'image Im(xi ,yj ) en un point (xi ,yj ) s'effectue de façon connue par l'intégration des signaux reçus dans un temps d'analyse T. L'image Im(xi ,yj ) est alors donnée par la relation suivante : Im x i , y j = 0 T I t + iQ t . exp i 4 π λ L x i , y j , t s t

Figure imgb0001
L(xi ,yj ,t) est la distance entre la source rayonnante 11, 12 à l'instant t et le point d'analyse (xi ,yj ) sur l'individu, λ représentant la longueur d'onde. Les distances L(xi ,yj ,t) sont délivrées par la caméra 5. s(t) représente la distance entre le centre de l'antenne émettrice et la caméra.The formation of the image Im ( x i , y j ) at a point ( x i , y j ) is effected in a known manner by the integration of the signals received in an analysis time T. The image Im ( x i , y j ) is then given by the following relation: im x i , there j = 0 T I t + iQ t . exp - i 4 π λ The x i , there j , t - s t
Figure imgb0001
Where L ( x i , y j , t ) is the distance between the radiating source 11, 12 at time t and the point of analysis ( x i , y j ) on the individual, where λ is the length of wave. The distances L ( x i , y j , t ) are delivered by the camera 5. s (t) represents the distance between the center of the transmitting antenna and the camera.

Avantageusement, la caméra permet de réaliser autour de l'individu visé une enveloppe virtuelle dont on connaît les distances au dispositif selon l'invention. Cette enveloppe virtuelle correspond en fait à la surface extérieure des vêtements portés par l'individu. Elle permet d'obtenir une surface de référence. Les mesures effectuées par la caméra permettent en fait d'obtenir un réseau maillé représentant cette surface. La surface peut être obtenue par lissage en effectuant une moyenne. Cette surface est calculée à intervalles de temps réguliers, par exemple toutes les 20 ms, permettant de focaliser sur chaque partie de l'individu en mouvement (bras, torse, jambes ...).
La caméra qui peut être du type infrarouge, ayant une rétine constituée d'un réseau de capteurs CMOS mesure la distance par le niveau de puissance reçue. Pour un codage réalisé sur 12 bits par exemple, la précision de mesure peut-être de 1 millimètre à une distance d'un mètre.
Advantageously, the camera makes it possible to produce around the target individual a virtual envelope whose distances to the device according to the invention are known. This virtual envelope corresponds in fact to the outer surface of the clothes worn by the individual. It makes it possible to obtain a reference surface. The measurements made by the camera make it possible to obtain a mesh network representing this surface. The surface can be obtained by smoothing by averaging. This surface is calculated at regular time intervals, for example every 20 ms, to focus on each part of the individual in motion (arms, torso, legs ...).
The camera, which may be of the infrared type, having a retina consisting of a network of CMOS sensors measures the distance by the received power level. For a coding carried out on 12 bits for example, the measurement accuracy can be of 1 millimeter at a distance of one meter.

La figure 10 illustre la détection d'un objet 103 à travers un vêtement 101, l'objet étant fixé sur le corps 102 de l'individu en dessous du vêtement 101. La distance du vêtement, plus particulièrement de ses points, est mesurée et connue du dispositif selon l'invention, le vêtement ayant été représenté comme la surface virtuelle tel que décrit précédemment. L'obtention de cette enveloppe est très importante car elle permet de suivre les déformations du vêtement dues au corps en mouvement. En effet, la caméra 5 permet la mesure de distance selon des périodes de temps données, par exemple toutes les 20 ms, de toutes les parties du corps en mouvement, plus précisément de l'enveloppe vestimentaire. Ces mesures de distance permettent la formation d'un filtre adapté pour la formation des images.The figure 10 illustrates the detection of an object 103 through a garment 101, the object being fixed on the body 102 of the individual below the garment 101. The distance of the garment, more particularly from its points, is measured and known to the device according to the invention, the garment having been represented as the virtual surface as described above. The obtaining of this envelope is very important because it makes it possible to follow the deformations of the garment due to the body in movement. Indeed, the camera 5 allows distance measurement according to given periods of time, for example every 20 ms, of all moving parts of the body, more specifically of the clothing envelope. These distance measurements allow the formation of a suitable filter for the formation of images.

Le processus de formation d'image s'effectue selon deux étapes : une étape d'acquisition et une étape de focalisation. Dans l'étape d'acquisition, le radar acquiert les composantes I et Q de l'équation (1) ci-dessus. Etant donné que les signaux radar traversent les vêtements, l'image acquise est celle du corps équipé éventuellement d'un objet 103. La détermination des coefficients de réflexions des signaux reçus permet de définir classiquement la nature des parties de l'image et notamment de l'objet 103.
Dans l'étape de focalisation, la caméra permet de définir les distances formant l'argument de l'exponentielle de l'intégrale dans l'équation (1) et donc de calculer l'image.
La résolution de l'image est égale à λ . F 2 D .

Figure imgb0002

L'image obtenue est donnée par la relation (1). Pour chaque pixel x, y de l'image on procède au calcul : I t + iQ t . exp i 4 π λ L x i , y j , t s t
Figure imgb0003
la partie exp i 4 π λ L x i , y j , t s t
Figure imgb0004
correspondant au filtre adapté. (L(xi ,yj ,t)) est calculée sur la surface virtuelle formée à partir de plusieurs points mesurés sur les vêtements, sur chaque partie du corps de l'individu en mouvement.
Le bruit causé par les imprécisions de mesures est classiquement filtré par des fenêtres glissantes sur l'image.The imaging process is performed in two steps: an acquisition step and a focusing step. In the acquisition step, the radar acquires the I and Q components of equation (1) above. Since the radar signals pass through the garments, the acquired image is that of the body possibly equipped with an object 103. The determination of the reflection coefficients of the received signals makes it possible to classically define the nature of the parts of the image and in particular of the object 103.
In the focusing step, the camera makes it possible to define the distances forming the argument of the exponential of the integral in equation (1) and thus to calculate the image.
The resolution of the image is equal to λ . F 2 D .
Figure imgb0002

The image obtained is given by relation (1). For each pixel x, y of the image, proceed to the calculation: Σ I t + iQ t . exp - i 4 π λ The x i , there j , t - s t
Figure imgb0003
the part exp - i 4 π λ The x i , there j , t - s t
Figure imgb0004
corresponding to the adapted filter. ( L ( x i , y j , t )) is calculated on the virtual surface formed from several points measured on the clothes, on each part of the body of the moving individual.
The noise caused by measurement inaccuracies is conventionally filtered by slippery windows in the image.

L'image finale est obtenue selon la relation (1) et est calculée par le calculateur 6 à partir de l'image fournie par le radar, par les composantes I et Q, et de l'image fournie par la caméra délivrant l'argument de l'exponentielle. Dans un mode de réalisation possible, le calculateur 6 peut être intégré dans le radar 2. En particulier la fonction du calculateur 6 peut être réalisée par les moyens de traitement du radar qui traitent les composantes I et Q de l'image SAR.
Une fois l'image finale obtenue, la reconnaissance et la classification des objets peut être réalisée en analysant :

  • Leurs formes ;
  • Leurs permittivités diélectriques, révélant leurs natures.
Cette reconnaissance peut être réalisée par le calculateur 6 ou les moyens de traitement du radar.The final image is obtained according to the relation (1) and is calculated by the computer 6 from the image supplied by the radar, the I and Q components, and the image supplied by the camera delivering the argument. the exponential. In a possible embodiment, the computer 6 can be integrated in the radar 2. In particular the function of the computer 6 can be performed by the radar processing means which process the components I and Q of the SAR image.
Once the final image has been obtained, object recognition and classification can be performed by analyzing:
  • Their forms;
  • Their dielectric permittivities, revealing their natures.
This recognition can be performed by the computer 6 or the radar processing means.

Dans un mode de réalisation particulier, le radar 2 émet selon plusieurs fréquences, proches d'une fréquence donnée, par exemple 77 GHz. Le radar 2 émet par exemple selon cinq fréquences F1, F2, F3, F4, F5. Dans la phase mesure, l'impulsion est par exemple découpée en cinq parties, les parties étant émises successivement à F1, F2, F3, F4, F5. Si l'impulsion dure 200 µs, chaque partie dure alors 40 µs.
Plus généralement, le radar émet en continu (CW), l'impulsion d'émission étant découpée en N parties, chaque partie correspondant à une fréquence. On reste par la suite dans l'exemple où N est égal à 5.
Dans la phase analyse, les phases et amplitudes sont par exemple calculées pour toutes les fréquences. Une première analyse à la première fréquence F1 est faite sur l'ensemble du corps. Puis une deuxième analyse est faite sur une zone limitée 110 contenant une forme détectée pour les quatre autres fréquences F2, F3, F4, F5, comme l'illustre la figure 11. Ces différentes analyses permettent de s'approcher de la valeur théorique de la permittivité diélectrique de l'objet et de son épaisseur.
In a particular embodiment, the radar 2 transmits at several frequencies, close to a given frequency, for example 77 GHz. The radar 2 emits for example according to five frequencies F1, F2, F3, F4, F5. In the measurement phase, the pulse is for example divided into five parts, the parts being emitted successively to F1, F2, F3, F4, F5. If the pulse lasts 200 μs, each part then lasts 40 μs.
More generally, the radar transmits continuously (CW), the emission pulse being divided into N parts, each portion corresponding to a frequency. We remain thereafter in the example where N is equal to 5.
In the analysis phase, the phases and amplitudes are for example calculated for all the frequencies. A first analysis at the first frequency F1 is done on the whole body. Then a second analysis is made on a limited area 110 containing a shape detected for the other four frequencies F2, F3, F4, F5, as illustrated by FIG. figure 11 . These different analyzes make it possible to approach the theoretical value of the dielectric permittivity of the object and its thickness.

A titre d'exemple, on peut atteindre des valeurs mesurées respectivement de 2,9 et 11 mm de la permittivité diélectrique et l'épaisseur pour des valeurs théoriques de 3,1 et 10 mm.By way of example, measured values of 2.9 and 11 mm respectively of the dielectric permittivity and the thickness for theoretical values of 3.1 and 10 mm can be achieved.

La figure 12 présente un exemple de réalisation d'un dispositif selon l'invention, portable. La partie antennaire constituée d'un ou deux scanners 1, 1', le radar 2 et leurs moyens d'interconnexion 3, 4, 83, 84 sont disposés à l'intérieur d'une structure cylindrique faisant également fonction de radôme 80. Cette structure supporte par ailleurs la caméra 5. La structure 80 est reliée à une poignée 120 permettant d'obtenir un dispositif portable, facilement maniable et léger. Son coût de réalisation peut être faible en raison du type de composants utilisés, en particulier le radar 2 peut être un radar de type automobile, économique, et la caméra peut-être de type Kinect, également économique. Les composants constituant le scanner intérieur (cylindres, guides d'onde, moteur et roulement à billes) sont également économiques.
On obtient ainsi un dispositif permettant la détection d'objets illicites en détectant les formes à travers les vêtements et en caractérisant leur matière. Il peut être utilisé en mouvement. La détection peut facilement se faire en pointant le dispositif à environ un mètre d'un individu à contrôler.
Le dispositif de détection est relié à des moyens de visualisation par une liaison sans fil adaptée. Les moyens de visualisation 7 peuvent être un écran disposé dans un centre de contrôle ou être à portée de l'utilisateur qui manipule le dispositif. Les moyens de visualisation peuvent également être des lunettes portées par l'utilisateur et sur lesquelles sont projetées les images détectées.
Il est possible de prévoir une deuxième caméra stéréoscopique pour améliorer le champ de vision.
The figure 12 shows an exemplary embodiment of a device according to the invention, portable. The antenna part consisting of one or two scanners 1, 1 ', the radar 2 and their interconnection means 3, 4, 83, 84 are arranged inside a cylindrical structure which also acts as a radome 80. structure also supports the camera 5. The structure 80 is connected to a handle 120 for obtaining a portable device, easily manageable and lightweight. Its realization cost may be low because of the type of components used, especially the radar 2 can be a car-type radar, economic, and the camera may be Kinect type, also economic. The components constituting the scanner interior (cylinders, waveguides, motor and ball bearings) are also economical.
This provides a device for detecting illicit objects by detecting forms through clothing and characterizing their material. It can be used in motion. The detection can easily be done by pointing the device to about one meter from an individual to control.
The detection device is connected to viewing means by a suitable wireless link. The visualization means 7 may be a screen disposed in a control center or be within the reach of the user who manipulates the device. The display means may also be glasses worn by the user and on which the detected images are projected.
It is possible to provide a second stereoscopic camera to improve the field of view.

La figure 13 présente un autre exemple d'utilisation d'un dispositif selon l'invention avec un autre « packaging ». Le système de contrôle est ici appliqué au niveau de portes 131, 132 s'ouvrant automatiquement. Quatre dispositifs selon l'invention, dont deux sont représentés par leurs radômes 80, peuvent être utilisés. Pour chaque porte, un dispositif est placé vers l'extérieur et un dispositif est placé vers l'intérieur, chaque dispositif étant placé au plus près de l'ouverture. Comme dans l'exemple de la figure précédente, un individu ou un objet mobile peut être contrôlé sous tous les angles. Un écran de visualisation, commun aux quatre dispositifs, est placé à distance.The figure 13 presents another example of use of a device according to the invention with another "packaging". The control system is here applied at doors 131, 132 opening automatically. Four devices according to the invention, two of which are represented by their radomes 80, can be used. For each door, a device is placed to the outside and a device is placed inward, each device being placed closer to the opening. As in the example of the previous figure, an individual or a moving object can be controlled from all angles. A display screen, common to all four devices, is placed at a distance.

Les exemples de réalisations précédents montrent que l'invention améliore la fluidité des contrôles, en particulier dans les lieux de passages, tels que par exemple les aéroports, les gares ou les centres commerciaux ou autres lieux publics.The examples of previous achievements show that the invention improves the fluidity of controls, especially in places of passage, such as for example airports, railway stations or shopping centers or other public places.

Claims (11)

  1. Device for detecting objects borne by immobile or moving individuals, characterized in that it includes at least:
    - at least one rotary antenna (1, 1') including at least two parallel rectilinear waveguides (24, 25) and a cylinder (21) provided with a helicoidal slot (22) rotatably movable about said guides, which guides are open facing the interior face of said movable cylinder, said surface forming a microwave short-circuit in order to close said guides, one of said guides (24) being dedicated to emission, a movable radiating source (11, 12) being located facing said guides subsequent to the rotational movement of said cylinder (21) inducing a movable emission and reception beam able to be oriented towards an individual;
    - one radar (2) emitting a continuous wave (CW) microwave signal towards the emission guide (24) of said antenna and receiving the signals received from the guides (24, 25) of said antenna, which signals are captured by said movable beam, said received signals being the direct component I and the quadrature component;
    - one stereoscopic video camera (5) that is oriented in the same direction as said movable beam and able to record the clothing envelope of said individual, said envelope serving as a reference surface for the measurement of distances to said device;
    - one processor (6) that computes an SAR image of that portion of the body of said individual which is targeted by said radar and said video camera and who is possibly equipped with one or more objects (103), from signals received from said radar (2) and the distances measured by said video camera (5).
  2. Device according to Claim 1, characterized in that the two guides (24, 25) being etched into a cylinder (26) placed in the interior of the movable cylinder (21), the two cylinders having the same axis (100), the space between the two cylinders is equal to 0.1 mm ± 0.05 mm.
  3. Device according to either one of the preceding claims, characterized in that said rotary antenna (1, 1') includes a system for minimizing microwave leaks, said system being composed of three cavities (52, 53, 53'), said cavities being arranged pairwise on each side of said waveguides (24, 25), parallelly thereto, over all their length.
  4. Device according to any one of the preceding claims, characterized in that said waveguides (24, 25) being etched into a cylinder (26) placed in the interior of the movable cylinder (21), said movable cylinder (21) and said interior cylinder (26) are rotatably movable by way of a ball bearing device (30), the base of said movable cylinder (21) and the base of said interior cylinder (26) being mechanically secured to the movable portion (27') and the stationary portion (27) of said device (30), respectively.
  5. Device according to any one of the preceding claims, characterized in that said radar (2) operates in a millimetre-wave frequency band.
  6. Device according to any one of the preceding claims, characterized in that it includes two rotary antennae (1, 1') so that said radar may operate in a bi-static mode, one antenna (1) realising the emission and the other antenna (1') being dedicated to the reception.
  7. Device according to Claim 6, characterized in that the antennae (1, 1') are connected together by two waveguides (83, 84), one guide (83) connecting the emission guides (24) of said antennae and the other guide (84) connecting the reception guides (25), the first waveguide (83) being connected via a magic T to a waveguide (3) that is connected to the radar and the second waveguide (84) being connected via another magic T to a waveguide (4) that is connected to the radar.
  8. Device according to any one of the preceding claims, characterized in that said radar (2) emits at a number N of frequencies close to a given frequency, the emission pulse being divided into N portions, each portion corresponding to one frequency, a first level of analysis of the image being performed for the signals received at the first of said frequencies (F1), other analyses being performed for the signals received at the other frequencies (F2, F3, F4, F5), the various analyses allowing the theoretical value of the dielectric permittivity of a detected object to be approached.
  9. Device according to any one of the preceding claims, characterized in that the processor (6) is an integral part of the processing means of said radar (2).
  10. Device according to any one of the preceding claims, characterized in that it includes means (7) for viewing the obtained images, said viewing means being glasses worn by a user and onto which said images are projected.
  11. Device according to any one of the preceding claims, characterized in that the antennal portion (1, 1'), the radar (2) and their interconnecting means (3, 4, 83, 84) are placed in the interior of a portable cylindrical structure (80) that also plays the role of a radome, said structure supporting said video camera (5).
EP17157293.6A 2016-02-24 2017-02-22 Device for detecting objects carried by an individual Active EP3211452B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1651492A FR3048088B1 (en) 2016-02-24 2016-02-24 DEVICE FOR DETECTING OBJECTS CARRIED BY AN INDIVIDUAL

Publications (2)

Publication Number Publication Date
EP3211452A1 EP3211452A1 (en) 2017-08-30
EP3211452B1 true EP3211452B1 (en) 2018-11-07

Family

ID=56741102

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17157293.6A Active EP3211452B1 (en) 2016-02-24 2017-02-22 Device for detecting objects carried by an individual

Country Status (4)

Country Link
US (1) US10641889B2 (en)
EP (1) EP3211452B1 (en)
CA (1) CA2958711A1 (en)
FR (1) FR3048088B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016124881B4 (en) * 2016-07-19 2019-11-07 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Apparatus and method for generating an image of an object with electromagnetic radiation
EP3762909A1 (en) * 2018-05-28 2021-01-13 Greenwave Systems PTE. LTD. Area monitoring and communication
EP3968045A1 (en) 2020-09-14 2022-03-16 Rohde & Schwarz GmbH & Co. KG Imaging system and method for material characterization of a sample

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2711440A (en) * 1944-10-09 1955-06-21 Rines Robert Harvey Microwave scanning system
US2694147A (en) * 1946-08-21 1954-11-09 Bell Telephone Labor Inc Scanning antenna system
US2670436A (en) * 1950-05-03 1954-02-23 Allen S Dunbar Helical slot scanner
GB0128659D0 (en) * 2001-11-30 2002-01-23 Qinetiq Ltd Imaging system and method
FR2855642B1 (en) * 2003-05-27 2005-07-08 Thales Sa ANTENNA, IN PARTICULAR FOR RADAR IMAGING, AND IMAGING DEVICE COMPRISING SUCH ANTENNA, IN PARTICULAR FOR THE DETECTION OF HIDDEN OBJECTS
US20060164286A1 (en) * 2005-01-21 2006-07-27 Safeview, Inc. Frequency-based surveillance imaging
IL186884A (en) * 2007-10-24 2014-04-30 Elta Systems Ltd System and method for imaging objects
ATE553397T1 (en) * 2008-12-30 2012-04-15 Sony Corp CAMERA-ASSISTED SCANNING IMAGING SYSTEM AND MULTI-ASPECT IMAGING SYSTEM
US8692708B2 (en) * 2010-03-30 2014-04-08 Sony Corporation Radiometric imaging device and corresponding method
US8670021B2 (en) * 2011-07-19 2014-03-11 Apstec Systems Ltd Method for stand off inspection of target in monitored space
US9304190B2 (en) * 2011-08-04 2016-04-05 Apstec Systems Ltd Method and system for unveiling hidden dielectric object
US9029778B1 (en) * 2011-11-04 2015-05-12 Telesecurity Sciences, Inc. Short standoff checkpoint detection system
FR3003959B1 (en) * 2013-04-02 2015-04-10 Sas Sws ROTARY ANTENNA, SCANNER USING SUCH ANTENNA, AND DEVICE FOR CONTROLLING PEOPLE
WO2015059132A2 (en) * 2013-10-21 2015-04-30 Sony Corporation Security system, method and device
US9575169B2 (en) * 2013-11-19 2017-02-21 Goodrich Corporation Rotating window and radome for surveillance pod

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
FR3048088B1 (en) 2018-02-16
EP3211452A1 (en) 2017-08-30
CA2958711A1 (en) 2017-08-24
FR3048088A1 (en) 2017-08-25
US20170242119A1 (en) 2017-08-24
US10641889B2 (en) 2020-05-05

Similar Documents

Publication Publication Date Title
EP2217944B1 (en) Device for detecting objects, particularly dangerous objects
EP2734851B1 (en) Calibration and testing device for an active antenna, particularly a nose-cone antenna of an airborne radar
EP3211452B1 (en) Device for detecting objects carried by an individual
Geibig et al. Compact 3D imaging radar based on FMCW driven frequency-scanning antennas
FR3058227A1 (en) FLEXW MULTIFUNCAL RADAR, IN PARTICULAR FOR AUTOMOBILE
EP2469299B1 (en) Method for enhancing images acquired by a radar with synthetic aperture
EP3001882B1 (en) Rotary antenna, scanner using such an antenna, and device for inspecting persons
FR2938925A1 (en) RADAR DEVICE FOR MARITIME SURVEILLANCE
EP2472215B1 (en) Method and device for the neutralisation of a target
EP0454582B1 (en) Radio direction finder antenna system with omnidirectional coverage
EP0852734B1 (en) Method and device for geodetic surveying and/or earth imaging by satellite signal processing
CA2840848C (en) Device for detecting objects such as mines
EP2737337B1 (en) Device for clutter-resistant target detection
EP0459886B1 (en) Distance-to-runway measuring device for a flying object
EP3775802A1 (en) Near-field terahertz imaging device
FR2855642A1 (en) Antenna for use in radar imagery device, has metallic cylinder with groups of waveguides where every group is associated to each of lays such that waveguide transmits on length of lay, different from another waveguide
Yocky et al. Bistatic SAR: Imagery & Image Products.
FR2550347A1 (en) Improvements to pulsed Doppler radars
EP2671089A1 (en) Method for measuring transmission frequencies using a rotary interferometer
FR2944605A1 (en) DEVICE FOR DETECTING OBJECTS INCLUDING, IN PARTICULAR, AN INDIVIDUAL
Henry et al. 3-D broadband terahertz synthetic aperture imaging
FR2972270A1 (en) Detection device for detecting dangerous objects e.g. weapons, in stream of individuals in e.g. public place, has two scanners placed on sides of conveyor belt to form radar image of portion of person
Dai et al. New development of high-resolution imaging for forward-looking SAR with multiple receiving antennas
FR2747790A1 (en) Orthogonal polarisation radar for detection of stationary targets

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20180214

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: G01S 7/03 20060101ALI20180424BHEP

Ipc: G01S 13/88 20060101AFI20180424BHEP

Ipc: G01S 13/90 20060101ALI20180424BHEP

INTG Intention to grant announced

Effective date: 20180523

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: AT

Ref legal event code: REF

Ref document number: 1062742

Country of ref document: AT

Kind code of ref document: T

Effective date: 20181115

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602017000787

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REG Reference to a national code

Ref country code: CH

Ref legal event code: PK

Free format text: RECTIFICATIONS

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: SWS

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 602017000787

Country of ref document: DE

Owner name: SWS, FR

Free format text: FORMER OWNERS: CHEKROUN, CLAUDE, GIF-SUR-YVETTE, FR; CHEKROUN, GILLES, GIF SUR YVETTE, FR

RIN2 Information on inventor provided after grant (corrected)

Inventor name: CHEKROUN, GILLES

Inventor name: CHEKROUN, CLAUDE

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20181107

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1062742

Country of ref document: AT

Kind code of ref document: T

Effective date: 20181107

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190307

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190207

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190207

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190307

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190208

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602017000787

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20190808

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190222

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20190228

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190222

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190228

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200229

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200229

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20170222

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181107

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20230208

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20230202

Year of fee payment: 7

Ref country code: DE

Payment date: 20230207

Year of fee payment: 7

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602017000787

Country of ref document: DE

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20240222